Cryogenic fuel power system

ABSTRACT

A cryogenic fuel power system includes an engine. The cryogenic fuel power system includes a cryogenic fuel supply that supplies cryogenic fuel to be used as fuel by the engine. The cryogenic fuel power system includes a cryogenic bus configured to provide the cryogenic fuel from the cryogenic fuel supply to the engine. The cryogenic fuel power system includes power electronics circuitry that converts power from the engine into a form to be applied to one or more loads. The power electronics circuitry is positioned in thermal communication with the cryogenic bus to transfer heat from the power electronics circuitry to the cryogenic fuel.

BACKGROUND

The subject matter disclosed herein relates to power systems, and moreparticularly, to a multilevel inverter that converts power for cryogenicpower systems.

Cryogenic power systems, as used herein, are those that include acryogenic fuel used by an engine to produce power. For instance,cryogenic fuel may be stored as a liquid and, to be used, may beprovided to a vaporizer that vaporizes the fuel to be used by theengine. The engine may then combust the vaporized fuel to producemechanical power that may then be converted to electrical power. Theelectrical power may then be converted to a form suitable for poweringone or more loads using power electronics circuitry.

Cryogenics may be used in a wide variety of applications, such asautomotive, locomotive, aerospace, or stationary, among others. In someof these applications, less weight and/or space occupied by thecryogenic power system may result in increased power density. However,some of the components, such as the vaporizer and the power electronicscircuitry, may increase the size and/or weight of the cryogenic powersystem.

BRIEF DESCRIPTION

In one embodiment, a cryogenic fuel power system includes an engine, acryogenic fuel supply that supplies cryogenic fuel to be used as fuel bythe engine, a cryogenic bus that provides the cryogenic fuel from thecryogenic fuel supply to the engine, and power electronics circuitrythat converts power from the engine into a form to be applied to one ormore loads, wherein the power electronics circuitry is positioned inthermal communication with the cryogenic bus to transfer heat from thepower electronics circuitry to the cryogenic fuel.

In another embodiment, a method includes flowing a cryofuel from acryofuel storage to an engine configured to combust a gas generated fromthe cryofuel, between the cryofuel storage and the engine, flowing thecryofuel proximate to power electronics circuitry to reduce atemperature at which the power electronics circuitry operates, andoperating the cooled power electronics circuitry to convert electricalpower generated by the combustion of the gas by the engine into a formto be applied to one or more loads.

In another embodiment, a power system includes a vaporizer configured toreceive cryofuel and to vaporize the cryofuel into a gas, an engineconfigured to receive the gas and to produce rotational energy to beconverted to electrical power, a cryofuel supply configured to providecryofuel to the vaporizer, power electronics circuitry configured toconvert the electrical power into a form to be applied to one or moreloads, wherein the power electronics circuitry is configured to bepositioned in thermal communication with the cryofuel to transfer heatproduced from operation of the power electronics circuitry to thecryogenic fuel.

BRIEF DESCRIPTION OF THE DRAWINGS

These and other features, aspects, and advantages of the presentinvention will become better understood when the following detaileddescription is read with reference to the accompanying drawings in whichlike characters represent like parts throughout the drawings, wherein:

FIG. 1 is a block diagram of a cryogenic fuel (cryofuel) power systemhaving power electronics circuitry cooled by the cryofuel prior to thecryofuel entering a vaporizer, in accordance with aspects of the presentdisclosure;

FIG. 2 is a block diagram of the power electronics circuitry of FIG. 1having a single unit of a multilevel inverter, in accordance withaspects of the present disclosure;

FIG. 3 is a schematic diagram of the single unit of a multilevelinverter of FIG. 2, in accordance with aspects of the presentdisclosure;

FIG. 4 is a block diagram of a set of units from FIG. 3 in a multilevelinverter, in accordance with aspects of the present disclosure;

FIG. 5 is a graph of output voltages of each of the units of FIG. 4which form a summation waveform, in accordance with aspects of thepresent disclosure;

FIG. 6 is another graph of output voltages of each of the units of FIG.4 which form another summation waveform, in accordance with aspects ofthe present disclosure;

FIG. 7 is a block diagram of four units of FIG. 3 in a multilevelinverter, in accordance with aspects of the present disclosure; and

FIG. 8 is a block diagram of output voltages of three multilevelinverters of FIG. 7 that provide three phase power to one or more loads,in accordance with aspects of the present disclosure.

DETAILED DESCRIPTION

The subject matter disclosed herein relates to power electronicscircuitry for use in cryogenic power systems that utilize cryogenic fuelto produce electrical power. Cryogenic fuel (cryofuel), as used herein,refers to fuel stored at temperatures at which the fuel is in a liquidstate (i.e., below its boiling point at a given pressure), such asliquefied natural gas (LNG) Hydrogen and others. In conventionalsystems, the liquid cryofuel may flow from a supply or storage to avaporizer that heats (or reduces the pressure of) the fuel to transformthe fuel from the liquid state into a gaseous state. The gaseous fuelmay then be provided to an engine, such as an internal combustionengine, which combusts the gas to generate mechanical motion. Themechanical motion may drive a generator to produce electric power. Powerelectronics circuitry of the cryogenic power system may convert theelectric power into a form suitable to be applied to one or more loads.Further, the power electronics circuitry may include hardware, such as acompressor, heat exchanger, among others, to control the temperature ofthe power electronics circuitry.

The size and/or weight of the vaporizer may depend on the amount of heatand/or expansion volume that is used in the gasification process toconvert the cryofuel from a liquid to a gas. That is, the larger thevaporizer, the more heat and/or expansion space the vaporizer mayprovide to the cryofuel. As such, the vaporizer may take up an amount ofspace and weight suitable to vaporize the cryofuel to a specified volumeor flow rate gaseous fuel. Similarly, the designed size of the powerelectronics circuitry depends on the amount of power and energycontrolled from the power electronics circuitry. As power density refersto the amount of power conditioned per unit weight or volume, it isdesirable to reduce the amount of space occupied by the vaporizer aswell as reduce the amount of space occupied by the power electronicscircuitry to improve the power density. Likewise it is of interest todecrease the weights of these elements to further improve the overallpower density.

Embodiments of the present disclosure improve the power density of thecryogenic power system by transferring heat from the power electronicscircuitry to the cryofuel to increase the temperature of the cryofuelwhile being transported to the vaporizer while simultaneously reducingthe temperature of the power electronics. That is, present embodimentsmay include a conduit from the cryofuel supply to an enclosure of thepower electronics circuitry to cool the power electronics circuitry andto heat the cryofuel as it flows toward the vaporizer. Thus theenclosure may include a conduit to provide the cryofuel to the vaporizer(after cooling the power electronics) at a temperature greater thanwould occur if the cryofuel were instead directly routed to thevaporizer, without cooling the power electronics. As such, the vaporizermay be of a reduced size, or even eliminated, due to the heating of thecryofuel by the power electronics circuitry.

Further, the power electronics circuitry operated at cryogenictemperatures occupies much less volume (and weighs less) than powerelectronics circuitries operated at high temperatures that process thesame quantity of power.

Further, the power electronics circuitry may include circuitry of areduced size due to operating the power electronics circuitry at atemperature lower than would occur if not cooled by the flow ofcryofuel. For example, the power electronics circuitry may be reduced insize by not including a compressor or heat exchanger (or using a smallercompressor or heat exchanger than would otherwise be the case) due tothe cooling provided by the flow of cryofuel. As such, the power densityof the cryogenic power system may be improved by reducing the size ofthe vaporizer and/or the power electronics circuitry.

Moreover, in some embodiments, the power electronics circuitry mayinclude circuitry that provides electric power to the one or more loadswithout an output filter to improve the efficiency of the cryogenicpower system as well as further reducing its size. That is, conventionalinverters may use passive filtering to provide power to the one or moreloads. However, the passive filter may include an inductor large enoughthat the cryogenic temperature can affects its magnetic field and theones produced by other inductors embedded in the cryogenic power system,thereby decreasing the efficiency of the cryogenic power system. Assuch, the power electronics circuitry of present embodiments may providepower output with much reduced or even without the use of passivefiltering.

To provide power conversion without the use of a passive filter, thepower electronics circuitry may include at least two resonant phasesthat divide input power over each of the resonant phases. The powerelectronics circuitry may include a transformer for each of the phases.For example, each of the resonant phases may be coupled to primarywindings of a respective transformer. Secondary windings of each of thetransformers may be coupled to a respective controlled rectifier. Bysplitting the power conversion over multiple phases, power through eachof the phases may be reduced, thereby allowing for the use of componentsthat are designed to withstand less power on each phase. Each of thephases may include circuitry to provide a portion of a total poweroutput based on a reference output. By dividing power over multiplephases, the power electronics circuitry may provide power at steps thatdo not include frequencies of harmonics that were filtered by passivefilters.

With the preceding introductory comments in mind, FIG. 1 shows a blockdiagram of a cryogenic fuel (cryofuel) power system 10 that uses cooledfuel, such as liquefied natural gas, stored at temperatures at which thefuel is in a liquid state. The cryofuel power system 10 may include acryofuel supply 12, such as a cryofuel tank which may be insulated oractively cooled. The cryofuel power supply 10 may further include acryogenic bus 15 having a conduit 16 that provides liquid cryogenic fuelfrom the cryofuel supply 12 to a vaporizer 14 to be gasified. Thevaporizer 14 may provide heat (and/or reduced pressure in the form ofexpansion space) to the liquid fuel to vaporize the fuel into a gas 18.An engine 20 may receive the gas and combust the gas 18 to producemechanical motion. The engine 20 may be any engine suitable forproviding mechanical motion from vaporized cryofuel, such as an internalcombustion engine, gas engine, or the like. The mechanical motion maythen be converted to electrical power via a generator.

The cryofuel power system 10 may include power electronics circuitry 22described below to convert the electrical power to a form suitable forpowering one or more loads in various applications, such as powering apower grid, a locomotive, a vehicle (e.g., a truck, a car, a ship, or anairplane). The cryofuel power system 10 includes one or more connections24 (e.g., power, control, communication, or logic connections) toprovide the power electronics circuitry 22 with power, control,communication, logic, or any combination thereof. The cryofuel powersystem 10 further includes one or more connections 26 (e.g., power,control, communication, or logic connections) to provide power to theone or more loads.

In some of these applications, it may be desirable to improve the powerproduced per unit mass of the cryofuel system, referred to as the powerdensity, without reducing the efficiency of the system. During the powerconversion process, the power electronics circuitry 22 may produce anamount of heat due to electrical resistances and/or impedances presentin the system during operation. The heat may reduce the efficiency ofthe power electronics circuitry 22 and increase the wear on thecircuitry. As such, some embodiments of the cryofuel power system 10 mayinclude additional hardware, such as fans, heat exchangers, or the like,to reduce the heat on the power electronics circuitry 22 or to otherwisemaintain the thermal environment of the power electronics circuitry 22within certain specified operational bounds.

Moreover, the vaporizer 14 may be designed to be of a size and/or powersufficient to provide an amount of heat or volume sufficient to vaporizea working volume or flow rate of the natural gas from a liquid state toa gaseous state during operation. Thus, the volume and/or mass of thevaporizer 14 may depend, at least in part, on the temperature of thenatural gas prior to entering the vaporizer and the desired temperatureof the natural gas after heating. That is the differential between theinlet temperature of the liquid fuel and the outlet temperature of thevaporized fuel during operation will typically determine the operationalparameters designed into the vaporizer, such as volume (e.g., size)and/or heat generating capacity. As such, the cryofuel power system 10typically includes a vaporizer 14 that is of a size and power to provideheat to heat the natural gas from a temperature of the supplied naturalgas to a temperature suitable for operations of the engine 20. However,both the additional hardware to cool the power electronics circuitry andthe size and power of the vaporizer 14 reduce the power density of thecryofuel power system 10.

In accordance with the present approach, the heat generated by theoperation of the power electronics circuitry 22 is used to heat orpre-heat the fuel (e.g., liquefied natural gas) prior to entering thevaporizer 14. This, thereby reduces the differential between the entry(i.e., inlet) and exit (i.e., outlet) temperature of the fuel withrespect to the vaporizer, and thus reduces the degree to which the fuelis heated in the vaporizer to achieve the desired expansion to a gas.

By way of example, the cryogenic bus 15 may include an enclosure thatincludes a housing of the power electronics 22. The enclosure 28 iscoupled between the conduit 16 and the vaporizer 14. The housing of thepower electronics circuitry 22 may be positioned proximate to thecryogenic bus 15 to transfer heat from the power electronics circuitryto the cryogenic fuel when the fuel flows to the vaporizer 14. In theillustrated embodiment, the housing of the power electronics ispositioned within the enclosure such that heat may be transferredbetween the housing and the cryofuel. That is, the enclosure 28 receivesthe liquid cryofuel from the conduit 16 at an inlet 30 and heat fromoperation of the power electronics circuitry 22 is transferred to (i.e.,heats) the fuel to reduce the operating temperature of the powerelectronics circuitry 22 while increasing the temperature of thecryofuel. While housing the power electronics circuitry 22 within theenclosure is used as an example, any suitable method of cooling thepower electronics using the cryofuel may be used. The natural gas mayexit the enclosure 28 via the outlet 32 that couples the vaporizer 14 tothe enclosure 28. While the embodiment described above includes anenclosure to remove heat from the power electronics 22, in otherembodiments, the power electronics may be directly cooled by beingsubmerged within the cryofuel.

By reducing the temperature of the power electronics circuitry 22 usingthe cryofuel (i.e. liquefied natural gas), hardware components that areotherwise used to cool the power electronics circuitry 22 may be reducedor eliminated. Further, by heating the cryofuel (i.e. liquefied naturalgas) prior to entering the vaporizer 14 using the heat from the powerelectronics circuitry 22, the cryofuel power system 10 may eliminate orreduce the size and/or power of the vaporizer 14 as compared to avaporizer 14 that is sized to provide all of the heat needed to vaporizethe fuel, i.e., heat without the added heat from the power electronicscircuitry 22. Additionally and/or alternatively, the vaporizer 14 mayuse less energy due to the heat from the power electronics circuitry 22raising the temperature of the fuel entering vaporizer 14 from what itwould otherwise be.

In the cryofuel power system 10, circuitry that includes materials thatcreate a magnetic field may have increased losses due to the lowtemperature associated with cryogenics. For example, conventionalinverters may include a passive filter to filter the output and toreduce total harmonic distortion (THD). However, passive filters mayinclude an inductor that creates a magnetic field which interacts withthe cryofuel, increasing losses of the power electronic circuitry 22and, consequently, of the power system 10. As such, the powerelectronics circuitry 22 described below may provide electrical power toone or more loads with reduced or eliminated magnetic materials. Forinstance, the power electronics circuitry 22 may operate without the useof a passive filter (e.g., that filters the output of the inverter)while creating minimal THD.

FIG. 2 shows a block diagram of a unit block 38 of the power electronicscircuitry 22. The power electronics circuitry 22 may receive power viathe connections 24. The power electronics circuitry 22 may include anactive filter 40 that filters the input power. The power electronicscircuitry 22 may include an N-phase resonant circuit 42 that receivesthe power from the active filter 40 and divides the power into N-phases.The number of phases may depend on the application, and N-phases refersto any suitable number of phases. Each phase of the N-phase resonantcircuit 42 may be electrically coupled to primary windings of arespective phase of the N-phase transformer 44. The power electronicscircuitry 22 may include an N-phase controlled rectifier 46 thatprovides the power output to the connections 26. Each phase of theN-phase controlled rectifier 46 may be electrically coupled to arespective secondary winding of the N-phase transformer 44. The powerelectronics circuitry 22 may include a slave controller 48 that controlsoperation of the N-phase resonant circuit 42 and/or the N-phasecontrolled rectifier 46.

The slave controller 48 may be electrically coupled to the powerelectronics circuitry 22 to receive and/or provide signals to controlvarious parts of the power electronics circuitry 22. For example, theslave controller 48 may include a sensor that receives a first signalindicating the power output of the connections 26. Further, the slavecontroller 48 may send signals to control operation of the N-phaseresonant circuit 42 and/or the N-phase controlled rectifier 46. Furtherit may include an output current sensor as well as an input voltagesensor. Furthermore, the slave controller 48 may receive a referencesignal (voltage, current and/or power) from a master control.

FIG. 3 shows a circuit diagram of an embodiment of the unit block 38 ofthe power electronics circuitry 22. The phases below may refer to thelegs or set of circuitry that may be included N number of times. Whiletwo phases are described in detail with respect to FIG. 3, note that theillustrated embodiment includes any suitable number of phases dependentupon the application. The N-phase resonant circuit 42 of the powerelectronics circuitry 22 includes at least two phases, referred to hereas a first phase resonant circuit 50 and a second phase resonant circuit52. The first phase resonant circuit 50 includes a first switch 54 and asecond switch 56, as well as a capacitor 58 and an inductor 60. Thesecond phase resonant circuit 52 includes a first switch 62 and a secondswitch 64, as well as a capacitor 66 and an inductor 68. In someembodiments, the first phase resonant circuit 50 and/or the second phaseresonant circuit 52 may include a capacitor without an inductor, or aninductor without the capacitor.

The first phase resonant circuit 50 may be electrically coupled toprimary windings 70 of a first transformer. In certain embodiments, thetransformer may include capacitance and/or inductance in place of aseparate capacitor and/or inductor. For example, the first phaseresonant circuit 50 may be electrically coupled to the primary windings70 without the inductor 60 and/or the capacitor 58. The second phaseresonant circuit 52 may be electrically coupled to primary windings 72of a second transformer.

In the illustrated embodiment, the primary windings 70 and 72 of eachphase resonant circuit 50 and 52 may induce a voltage in secondarywindings 78 and 80, respectively. Further, the secondary windings 78 and80 may be electrically coupled to a first phase controlled rectifier 82and a second phase controlled rectifier 84 of the N-phase controlledrectifier 46. The first phase controlled rectifier 82 may include afirst switch 86 and a second switch 88, and the second phase controlledrectifier 84 may include a third switch 90 and a fourth switch 92.Additionally, the N-phase controlled rectifier 46 may be coupled to acapacitor 94.

By coupling the first transformer between the first phase resonantcircuit 50 and the first phase controlled rectifier 82, the transformermay galvanically isolate power of the first phase resonant circuit 50from power of the first phase controlled rectifier 82. Similarly, bycoupling the second transformer between the second phase resonantcircuit 52 and the second phase controlled rectifier 82, the secondtransformer may galvanically isolate power of the second phase resonantcircuit 52 from power of the second phase controlled rectifier 82. Asmentioned above, the transformers may include numbers of windings tostep up or step down the voltages provided by the transformers to thecontrolled rectifiers.

Each phase may have hardware similar or identical to hardware of theother phases. In the illustrated embodiment, the capacitor 58 has acapacitance equal to the capacitance of a capacitor 66, and the inductor60 has an inductance equal to the inductance of an inductor 68. Further,each of the transformers may have a similar or identical relationship ofprimary windings 70 and 72 to secondary windings 78 and 80. Furthermore,switches 82 and 84 of each of the phases of the N-phase controlledrectifier 46 may be similar or identical to respective switches 86 and88 of other phases of the N-phase controlled rectifier 46.

In certain embodiments, the slave controller 48 may include variouscircuitry to perform the methods described herein. As an example, theslave controller 48 may include a processor 96 or multiple processors,memory 98, and/or a field programmable gate array (FPGA) and/or acomplex programmable logic device (CPLD). The slave controller 48 mayinclude circuitry and/or instructions to control the each of theN-phases, as shown by the first phase circuitry 100 and second phasecircuitry 102. The slave controller 48 may operate as a master over thefirst phase circuitry 100 and the second phase circuitry 102. Theprocessor may be operatively coupled to the memory to executeinstructions for carrying out the presently disclosed techniques, suchas controlling operation of the switches 54, 56, 62, 64, 86, 88, 90, and92. These instructions may be encoded in programs or code stored in atangible non-transitory computer-readable medium, such as the memoryand/or other storage. The processor may be a general purpose processor,system-on-chip (SoC) device, or application-specific integrated circuit,or some other processor configuration.

Memory 98, in the embodiment, may include a computer readable medium,such as, without limitation, a hard disk drive, a solid state drive, adiskette, a flash drive, a compact disc, a digital video disc, randomaccess memory (RAM), firmware, read only memory (ROM, EPROM, flashmemory, etc.) and/or any suitable storage device that enables processorto store, retrieve, and/or execute instructions (e.g., code) and/ordata. Memory 98 may also include one or more local and/or remote storagedevices.

The slave controller 48 may receive control signal(s) from a mastercontroller 123, described in detail below. For example, the mastercontroller 123 may receive a reference signal indicating a desiredoutput, such as a signal of a power grid. Further, the master controller123 may receive a sensor signal from a sensor 106 (e.g., voltage and/orcurrent sensor) indicating the power output on the connections 26.Alternatively and/or additionally, the slave controller 48 may receivesignals from the sensor 106. As described in detail below, the mastercontroller 123 may send signal(s) to the slave controller 48 to causethe slave controller 48 to control the switches to output power based onthe reference signal 104 and the sensor signal(s). The input power maythen be divided into N-phases via an N-phase resonant circuit 42. Bydividing the power between each of the phases, the power electronicscircuitry 22 may provide controlled power while minimizing losses byoperating at lower current per phase as compared to inverters that donot include N-phases. Moreover, by dividing the power into differentphases, the circuitry (e.g., switches, capacitors, inductors,transformers, etc.) on each of the phases may be rated to withstandreduced current and/or voltages as compared to power electronicscircuitry 22 that does not divide the power into different phases.Further, by limiting the output current of each phase, magnetic fieldsgenerated by current of the inverter may be limited, thereby reducinglosses of the power electronics circuitry 22 in cryofuel power systems10. In the illustrated embodiment, the output ripple frequency may beequal to 2N times the switching frequency, where N is the number ofphases of the N-phase. As such, the output ripple may be minimized basedon the switching frequency per phase and the number of phases. Further,a capacitor 107 may smooth the output of the inverter. Furthermore,because of the high ripple frequency, a filter inductor is much smalleror it could be removed completely compared to a traditional approach. Asdescribed below, more than one unit block 38 may be combined together toform a multi-level inverter of the power electronics circuitry 22. Themulti-level inverter 101 may be modular such that each of the unitblocks 38 are self-contained to enable changing of the multi-levelinverter 101 depending on the application.

FIG. 4 shows a multi-level inverter 101 having multiple unit blocks 103,107, 109, and 111. Although four unit blocks are shown in FIG. 4, thisis simply meant to be illustrative, and any suitable number of unitblocks may be used. Each of the unit blocks may include the powerelectronics circuitry 38 described above, such as the input activefilter 40, the N-phase resonant circuit 42, the N-phase transformer 44,the N-phase controlled rectifier 46, as well as the slave controller 48.

In the illustrated embodiment, unit block 103 is connected in series viaconnection 113 to unit block 107. Further, unit block 107 is connectedin series, via connection 115, to unit block 109, which is connected inseries via connection 117 to unit block 111. That is, the four unitblocks 103, 107, 109, and 111 are connected in series to one another toprovide an output voltage 119 with respect to ground.

The multi-level inverter 101 may include a master controller configuredto send signals to control the slave controllers of each of the unitblocks. While wiring is shown in FIG. 4, the master controller maycommunicate using any suitable communication technique or protocol(e.g., wireless or wired). Further, the master controller 127 mayinclude a processor 125 and a memory 127. The processor 125 and thememory 127 may be any suitable processor and memory (e.g., as describedwith respect to the slave controller 48). The memory 127 may includeinstructions to be executed by the processor 125 to perform thetechniques described herein.

The processor 125 may send control signals to each of the slavecontrollers of the unit blocks 103, 107, 109, and 111 to cause the slavecontrollers to control the switches of the respective unit block 103,107, 109, and 111 according to control signals of the master controller.The multi-level inverter 101 may provide power at a number of voltagelevels corresponding to the number of unit blocks coupled in series. Aswill be described below, the processor 125 may send control signals toeach of the slave controllers to control the switches of the respectiveunit blocks 103, 107, 109, and 111 to generate a summation waveformbased on the control signals.

Each of the unit blocks 103, 107, 109, and 111 may be coupled to thedirect current (DC) bus V_(DC). Further, the output of each unit block103, 107, 109, and 111 is galvanically isolated from the DC bus to floatthe output of each of the unit blocks 103, 107, 109, and 111 to enableseries output connection of multiple modules. That is, each of the unitblocks 103, 107, 109, and 111 may be galvanically isolated so that theseries connections 113, 115, and 117 form a summation voltage betweenthe voltage output 119 and ground 121 that combines each voltage outputof the unit blocks 103, 107, 109, and 111 (e.g., voltages acrossconnections 26 of each unit block 103, 107, 109, and 111). Further, bycoupling the unit blocks 103, 107, 109, and 111 with the seriesconnections, each of the phases of the unit blocks may be coupled inseries with one another such that voltages of each of the unit blocks.

FIG. 5 shows a graph 108 of output voltages, shown on the ordinate 110,with respect to time, shown on the abscissa 112, of the power outputfrom the multi-level inverter 101 of FIG. 4. The master controller 123,through the controllers 48, may control each of the N-phases of each ofthe unit blocks 103, 107, 109, and 111 to provide power output that maysum to form a sinusoidal waveform 114. The power electronics circuitry22 may include four unit blocks, each having N-phase resonant circuit, Ntransformers, and N controlled rectifiers. Each of the sections 116,118, 120, and 122 are shown to represent output voltages of each of theunit blocks 103, 107, 109, and 111. As mentioned above, the unit blocks103, 107, 109, and 111 may be modular, or the N-phases may be combined,depending on the circumstances.

The master controller may send signals to the slave controllers tocontrol operation of the switches of each of the resonant circuits toprovide a portion of alternating current (AC) power from the DC busV_(DC). For example, the slave controller 48 may control operation ofthe resonant circuit to provide power, as shown in section 116. Due tothe components of each of the resonant circuits (e.g., the inductor, thecapacitor, etc.) or the transformer, or the controlled rectifier, eachunit block 103, 107, 109, and 111 may provide a portion of the AC powerwith minimal harmonics and/or minimal voltage ripple without the use ofpassive filtering. For example, the first unit block 103 may be used toprovide a first portion of AC power provided by the first resonantcircuitry to include a reduced voltage ripple, a reduced ripplefrequency, or both. Similarly, the second unit block 107 may includesimilar or identical components to similarly shape the portion of ACpower provided by the second unit block 107 to include a reduced voltageripple, a reduced ripple frequency, or both, as compared to an inverterwithout the components of the resonant circuitry (e.g., the inductor,the capacitor, etc.). Further, by dividing the current through multiplephases, via the switches of the resonant circuits, magnetic fieldsgenerated by the inverter may be minimized to reduce impact of theinverter on the cryogenic fuel power system. That is, the slavecontroller may limit current through each of the resonant circuits toreduce or eliminate decreases in efficiency due to magnetic fields atlower temperatures due to the cryogenic fuel.

The master controller 123 may control each of the slave controllersbased on the reference signal 104 and the sensor signal. If the mastercontroller 123 determines that the voltage of the reference sinusoidalwaveform 114 is below a first threshold 124, then the master controllermay send signal(s) to the slave controller of the first unit block 103to control the first unit block 103 to provide a voltage based on thereference signal 104, and to the other unit blocks 107, 109, and 111 areference signal equal to 0. For example, the slave controller of thefirst unit block 103 may control (e.g., send signal(s) to open and/orclose) switches of each of the phases of the first unit block 103 togenerate an output voltage between time 0 and time t1, as shown bysection 116, and the slave controllers of every other unit will operatethe switches of the units to generate a zero-value output voltage. Whilethe reference signal 104 is between the first threshold 124 and a secondthreshold 126, the master controller 123 may send signal(s) to the slavecontroller of the first unit block 103 to keep a constant voltage equalto the threshold value, and to the slave controller 48 of the secondunit block 107 to control (e.g., send a signal to open) switches of thesecond unit block 107 to generate the output voltage between t1 and t2,shown by section 118. The unit blocks 109 and 111 will be controlled toproduce a zero-voltage output. Similarly, while the reference signal 104is between the second threshold 126 and a third threshold 128, themaster controller 123 may send signal(s) to the slave controller 48 ofthe third unit block 109 to control (e.g., send a signal to open)switches of the third unit block 109 to generate the output voltagebetween t2 and t3, as shown by section 120, and send signal(s) to theslave controller of unit blocks 103 and 109 to produce a constantvoltage equal to the threshold value, and to the slave control of unitblock 111 to produce a zero voltage output. The master controller 123may then send signal(s) to the slave controller 48 of the fourth unitblock 111 to control switches of the fourth phase to generate the outputvoltage between t3 and t4 while the reference signal is above the thirdthreshold 128, as shown by section 122 and send signal(s) to the slavecontrollers of unit blocks 103, 107 and 109 to produce a constant outputvoltage equal to the threshold voltage. The slave controller 48 maycontinue to control the switches to decrease the voltages in steps in asimilar manner such that the summation of each of voltages from each ofthe unit blocks forms the sinusoidal waveform 114. By increasing and/ordecreasing the voltages at steps using each of the unit blocks, theoutput from the power electronics circuitry 22 does not have harmonicsat frequencies that were conventionally filtered by a passive filter.Further, the resonant circuits of each of the phases may shape theportion of AC power provided by each of the phases, as shown by sections116, 118, 120, and 122, to include a reduced voltage ripple, a reducedripple frequency, or both, as compared to an inverter without thecomponents of the resonant circuitry.

While a sinusoidal waveform was used as a reference signal, the systemand methods described herein may be used with any suitable waveform as areference signal. FIG. 6 shows a graph 130 of an example of a trianglewaveform. While a triangle waveform and a sinusoidal waveform are usedhere as examples, the power electronics circuitry 22 may be used togenerate rectangular, sawtooth, or any other suitable waveform,including direct current (DC) and/or alternating current (AC) waveforms.Similar to FIG. 5, the master controller 123 may send signal(s) to theslave controllers 48 of each of the unit blocks to control each of thephases of the modular multilevel inverter 38 based on the referencesignal 104 and the sensor signal. That is, the master controller 123 maycompare the voltage of a reference triangle waveform to variousthreshold to control provide power via each of the phases. Power fromeach of these phases may be summed into a resultant signal.

FIG. 7 shows a block diagram of a set of unit blocks of an inverter 136that provides power output suitable to power one or more loads. Each ofthe unit blocks may include a slave controller 48, an input activefilter 40, an N-phase resonant circuit 42, an N-phase transformer 44,and an N-phase controlled rectifier 46. Further, each of the unit blocksmay be electrically coupled in series, in parallel, or any combinationthereof, to provide power at larger currents and/or voltages. That is,to increase the amount of current and/or voltage provided by the unitblocks of inverter, additional inverter units may be added in series, inparallel or any combination thereof.

In the illustrated embodiment, the inverter 136 includes a first unitblock 138 electrically coupled in parallel to a second unit block 140.The inverter 136 further includes a third unit block 142 electricallycoupled in parallel to a fourth unit block 144. The first unit block 138and the second unit block 140 are electrically coupled in series withthe third unit block 142 and the fourth unit block 144. That is, theinverter 136 includes a mix of two couples of inverter units in serieswith each couple having two units in parallel. Further, the unit blocksmay be modular to couple in series or in parallel due to the galvanicisolation of the transformers. By coupling unit blocks in parallel, theinverter may provide an increased total current to the load by dividingthe current through each of the phases of the unit blocks. By couplingadditional unit blocks in series, the inverter may provide power to theone or more loads at additional voltage levels. While this is shown asan example, a set of inverter units may be coupled in series, parallel,or a mix of both.

FIG. 8 shows a block diagram of three phase power system 146 thatprovides power using three inverters. For example, the first inverter136, a second inverter 148, and a third inverter 150 units may provide afirst phase, a second phase, and a third phase of power, respectively,to provide three phase power to a load.

Technical effects of the invention include improving power density, suchas in cryogenic power systems. By cooling power electronics usingcryofuel, the cryofuel is pre-heated prior to being heated by avaporizer, thereby reducing power used by the vaporizer. Further, bycooling the power electronics, the power electronics may operate withoutheat sinks and/or fans, thereby reducing the size of the powerelectronics. The power provided by the power electronics may operateusing a modular multilevel inverter. The multilevel inverter may dividepower through multiple modules. Further, each of the modules may includemultiple phases. A controller of each of the modules may controlswitches of the phases to form a summation waveform. By dividing thepower between multiple phases, the power electronics circuitry mayprovide power without the use of a passive filter, thereby reducinglosses caused by magnetic material of the passive filter. Further, byreducing magnetic materials and dividing the current through multiplephases, the inverter may enable cryogenic power systems to operate witha reduced size of a vaporizer as well as with reduced electronics.

The word switch, used in this description includes technologies such asIGBTs MOSFETs with or without the antiparallel diodes, as well asdifferent kind of material such as Silicon, Germanium, Silicon Carbide,Gallium Nitride etc. The switch in the rectifier portion can beunidirectional or bidirectional.

This written description uses examples to disclose the invention,including the best mode, and also to enable any person skilled in theart to practice the invention, including making and using any devices orsystems and performing any incorporated methods. The patentable scope ofthe invention is defined by the claims, and may include other examplesthat occur to those skilled in the art. Such other examples are intendedto be within the scope of the claims if they have structural elementsthat do not differ from the literal language of the claims, or if theyinclude equivalent structural elements with insubstantial differencesfrom the literal languages of the claims.

The invention claimed is:
 1. A cryogenic fuel power system, comprising:an engine; a cryogenic fuel supply configured to supply cryogenic fuelto be used as fuel by the engine; a cryogenic bus configured to providethe cryogenic fuel from the cryogenic fuel supply to the engine; powerelectronics circuitry configured to convert power from the engine into aform to be applied to one or more loads, wherein the power electronicscircuitry is positioned in thermal communication with the cryogenic busto transfer heat from the power electronics circuitry to the cryogenicfuel; wherein the cryogenic bus comprises a conduit and an enclosurethat includes a housing of power electronics circuitry, and wherein thecryogenic fuel tank provides cryogenic fuel to the enclosure to placethe housing of the power electronics circuitry in thermal communicationwith the cryogenic fuel; wherein the cryogenic power system comprises aplurality of unit blocks, wherein the cryogenic fuel power system isconfigured to divide power to a plurality of phases of each of the unitblocks of the plurality of unit blocks to power the one or more loads;and wherein an output ripple frequency is equal to 2N times a switchingfrequency of the power electronics circuitry where N is a number of theplurality of phases of each of the unit blocks.
 2. The cryogenic fuelpower system of claim 1, wherein the cryogenic fuel power systemcomprises a vaporizer in a fluid flow path between the cryogenic fuelsupply and the engine, wherein the vaporizer is sized based at least inpart on a temperature of the cryogenic fuel entering the vaporizer. 3.The cryogenic fuel power system of claim 1, wherein each phase of theplurality of phases comprises: a resonant circuit that provides aportion of AC power from a DC bus; a transformer that galvanicallyisolates the portion of the AC power between the resonant circuit and acontrolled rectifier; and the controlled rectifier that operates inconjunction with other controlled rectifiers of the plurality of phasesto generate a portion of a summation waveform of power to be applied tothe one or more loads.
 4. The cryogenic fuel power system of claim 3,wherein each unit block of the plurality of unit blocks comprises acontroller configured to control operation the resonant circuit, thecontrolled rectifier, or both.
 5. The cryogenic fuel power system ofclaim 1, wherein the cryogenic power system comprises a multilevelinverter configured to provide inverted power, without use of a passivefilter, to the one or more loads.
 6. The cryogenic fuel power system ofclaim 1, wherein the power electronics circuitry is submerged directlyin the cryogenic fuel.
 7. A method, comprising: flowing a cryofuel froma cryofuel storage to an engine configured to combust a gas generatedfrom the cryofuel; between the cryofuel storage and the engine, flowingthe cryofuel proximate to power electronics circuitry to reduce atemperature at which the power electronics circuitry operates; operatingthe cooled power electronics circuitry to convert electrical powergenerated by the combustion of the gas by the engine into a form to beapplied to one or more loads; wherein the power electronics circuitrycomprises a plurality of unit blocks, wherein the cryogenic fuel powersystem is configured to divide power to a plurality of phases of each ofthe unit blocks of the plurality of unit blocks to power the one or moreloads; and wherein an output ripple frequency is equal to 2N times aswitching frequency of the power electronics circuitry, where N is anumber of the plurality of phases of each of the unit blocks.
 8. Themethod of claim 7, wherein the cryofuel is heated en route to the engineby act of cooling the power electronics circuitry.
 9. The method ofclaim 7, wherein the power electronics circuitry converts direct current(DC) electrical power into alternating current (AC) electrical power tobe applied to the one or more loads.
 10. A power system, comprising: avaporizer configured to receive cryofuel and to vaporize the cryofuelinto a gas; an engine configured to receive the gas and to producerotational energy to be converted to electrical power; a cryofuel supplyconfigured to provide cryofuel to the vaporizer; power electronicscircuitry configured to convert the electrical power into a form to beapplied to one or more loads, wherein the power electronics circuitry isconfigured to be positioned in thermal communication with the cryofuelto transfer heat produced from operation of the power electronicscircuitry to the cryogenic fuel; wherein the power electronics circuitrycomprises a plurality of unit blocks, wherein the cryogenic fuel powersystem is configured to divide power to a plurality of phases of each ofthe unit blocks of the plurality of unit blocks to power the one or moreloads; and wherein an output ripple frequency is equal to 2N times aswitching frequency of the power electronics circuitry, where N is anumber of the plurality of phases of each of the unit blocks.
 11. Thepower system of claim 10, wherein the power electronics are configuredto preheat the cryofuel prior to entering the vaporizer.
 12. The powersystem of claim 10, comprising a conduit between the vaporizer and thecryofuel supply to transfer the cryofuel from the cryofuel supply to thevaporizer.
 13. The power system of claim 12, wherein the powerelectronics circuitry is configured to be submerged within the cryofuelalong the conduit.
 14. The power system of claim 12, wherein the powerelectronics circuitry is housed in a housing, the housing being inthermal communication with the cryofuel.
 15. The power system of claim10, wherein the power electronics circuitry is configured to providetransformed power to the one or more loads by dividing the power over aplurality of phases to limit current through each phase of the pluralityof phases, thereby limiting magnetic fields generated by the powerelectronics circuitry.
 16. The power system of claim 10, wherein thepower electronics is configured to convert the electrical power to forma sinusoidal waveform, a triangular waveform, a rectangular waveform ora DC waveform.
 17. The power system of claim 10, wherein each of theplurality of unit blocks provide a portion of a summation waveform to beapplied to the one or more loads.